%% Empty weight from historical data
%
% Index
%   1: turboprop single engine
%   2: turboprop twin engine
%   3: turbofan single engine
%


% Turboprop single engine
emptyWeightHistoricalCoeffs(1).A = 2.5597; % Analise de concorrentes
emptyWeightHistoricalCoeffs(1).c = -0.1785; % Analise de concorrentes
% emptyWeightHistoricalCoeffs(1).A = 2.36; % Raymer
% emptyWeightHistoricalCoeffs(1).c = -0.18; % Raymer

% Turboprop twin engine
emptyWeightHistoricalCoeffs(2).A = 0.1764; % Analise de concorrentes
emptyWeightHistoricalCoeffs(2).c = 0.1392; % Analise de concorrentes
% emptyWeightHistoricalCoeffs(2).A = 1,51; % Raymer
% emptyWeightHistoricalCoeffs(2).c = -0.1; % Raymer

% Turbofan
emptyWeightHistoricalCoeffs(3).A = NaN;
emptyWeightHistoricalCoeffs(3).c = NaN;
